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The Lycoming O-320 is a large family of naturally aspirated, 320 cu in (5.2 L) air-cooled, horizontally-opposed four-cylinder, direct-drive engines produced by Lycoming Engines. Introduced in 1953, it is commonly used on light aircraft such as the Cessna 172 and Piper Cherokee , and remains in production as of 2024.
The standard engine used is the 150 hp (112 kW) Lycoming O-320 powerplant. [ 1 ] [ 3 ] The Christavia Mk IV has a typical empty weight of 1,100 lb (500 kg) and a gross weight of 2,200 lb (1,000 kg), giving a useful load of 1,100 lb (500 kg).
By 1961, Lycoming produced 600 to 700 engines per month. [17] Its most successful post-war products were a series of air-cooled flat-4 and flat-6 general aviation engines. Most famous among these are the O-320 and O-360 four-cylinder engines, and the O-540 six-cylinder engine.
Data from Jane's All the World's Aircraft 1982-83 General characteristics Crew: 2 Length: 21 ft 2 in (6.45 m) Wingspan: 30 ft 0 in (9.14 m) Height: 7 ft 0 in (2.13 m) Wing area: 144 sq ft (13.38 m 2) Airfoil: NACA 43015 Empty weight: 1,125 lb (510 kg) Max takeoff weight: 1,817 lb (824 kg) normal category Fuel capacity: 35 US gal (29 imp gal; 130 L) Powerplant: 1 × Lycoming O-320-A2C 4 ...
The Diamant is a conventional, low-wing cantilever monoplane and essentially an enlarged version of Piel's successful Emeraude designed to accommodate more passengers. [1][2] This extra capacity is provided by a redesigned fuselage which is higher in the rear section and longer overall. [3] While the Emeraude has only two seats, side-by-side ...
Data from Brassey's World Aircraft & Systems Directory. General characteristics Crew: 2 Length: 24 ft 10 in (7.55 m) Wingspan: 34 ft 9 in (10.69 m) Height: 7 ft 9 in (2.36 m) Wing area: 136 sq ft (12.6 m 2) Airfoil: NACA 23015/23013 (root/tip) Empty weight: 1,750 lb (794 kg) Max takeoff weight: 2,550 lb (1,157 kg) Powerplant: 1 × Textron Lycoming AEIO-540-D 6-cylinder horizontally-opposed ...
The recommended engines for the Rebel are the 160 hp (120 kW) Lycoming O-320, the 116 hp (87 kW) Lycoming O-235 and the 80 hp (60 kW) Rotax 912, although Bayerl et al. note that the aircraft does not perform well with less than 100 hp (75 kW).
The Magnum was sold without an engine and was designed for a range of Lycoming engines from 115 to 180 hp (86 to 134 kW), for example the Lycoming O-235, O-320 or the O-360. [1] The enclosed cabin has side-by-side configuration seating for two with an option for an additional seat in the baggage area for two children or a small adult. [ 1 ]